View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 21797U 91081B 24282.57177990 .00000415 00000-0 39752-3 0 9997
2 21797 82.9523 238.5896 0038235 163.0017 247.7120 13.77748663651778
| Epoch (UTC): | 08 October 2024 13:43:21 |
| Eccentricity: | 0.0038235 |
| inclination: | 82.9523° |
| perigee height: | 944 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 238.5896° |
| argument of perigee: | 163.0017° |
| revolutions per day: | 13.77748663 |
| mean anomaly at epoch: | 247.7120° |
| orbit number at epoch: | 65177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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